Solid rocket stage. 1.00 kN (225 lbf) thrust.
Status: Retired 1972.
Unfuelled mass: 10 kg (22 lb).
Height: 1.70 m (5.50 ft).
Diameter: 0.0900 m (0.2950 ft).
Thrust: 1.00 kN (225 lbf).
Burn time: 4.00 s.
Number: 20 .
More... - Chronology...
Associated Countries
Associated Engines
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BB7 Bristol Aerospace solid rocket engine. 1 kN. More...
Associated Launch Vehicles
Associated Manufacturers and Agencies
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Bristol Canadian manufacturer of rocket engines and rockets. Bristol Aerospace Limited, Winnipeg, Manitoba, Canada. More...
Associated Propellants
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Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...
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